/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.0.x                                 |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/

FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    object      turbineProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

NumBl                   3;
TipRad                 0.075;
HubRad                  .0075;
UndSling                0.0;
OverHang               -.00001;
TowerHt                0.125;
Twr2Shft                0;
ShftTilt               0;
PreCone               0;
GBRatio                97.0;
GenIner               534.116;
HubIner               115.926E3;
BladeIner             11.776047E6;
//TorqueControllerType   "fiveRegion";
TorqueControllerType   "none";
YawControllerType      "none";
//PitchControllerType    "simpleLinear";
PitchControllerType    "none";


TorqueControllerParams
{
    CutInGenSpeed           670.0;
    RatedGenSpeed          1173.7;
    Region2StartGenSpeed    871.0;
    Region2EndGenSpeed     1161.963;
    CutInGenTorque            0.0;
    RatedGenTorque           43.09355E3;
    RateLimitGenTorque       15.0E3;
    KGen                      2.55764E-2;
    TorqueControllerRelax     1.0;
}


PitchControllerParams
{
    PitchControlStartPitch    0.0;
    PitchControlEndPitch      7.6;
    PitchControlStartSpeed    15.77;
    PitchControlEndSpeed      16.0;
    RateLimitPitch             4.5;
}



Airfoils
(
    "camberedPlate"
);


BladeData
(
!  radius(m)   c(m)     twist(deg) airfoil 
0.01      0.0139    20.50      0
0.02      0.0147    20.9       0
0.03      0.0147    19.83      0
0.04      0.0141    16.91      0
0.05      0.0131    13.19      0
0.06      0.0118    10.67      0
0.07      0.0102    9.12       0
0.075     0.0060    6.66       0
);
